書誌事項
- タイトル別名
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- Development of High Current Electron Emitter for Electric Propulsion
- デンキ スイシンキヨウ ダイ デンリュウ デンシ ゲン ノ サドウ トクセイ
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We have designed and manufactured a 100 A class electron emitter for high electric propulsion systems of space crafts. The electron emitter shape and materials were determined by the plasma analysis and the heat analysis. As the result of the operation test, the electron current of 100 A was successfully extracted. The operation reached to the steady-state within 10 sec in any case. In the low flow rate and high discharge current case, the discharge voltage was larger than other cases in order to extract the electron forcibly. In this case, the discharge voltage was fluctuated and a plume spread conically.
収録刊行物
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- プラズマ応用科学
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プラズマ応用科学 25 (1), 3-8, 2017
プラズマ応用科学会
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詳細情報 詳細情報について
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- CRID
- 1390846609783218944
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- NII論文ID
- 130007768825
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- NII書誌ID
- AA12687461
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- ISSN
- 24351555
- 13403214
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- NDL書誌ID
- 029324026
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可